U.S. patent number 10,876,745 [Application Number 15/633,042] was granted by the patent office on 2020-12-29 for air conditioning register.
This patent grant is currently assigned to TOYOTA JIDOSHA KABUSHIKI KAISHA. The grantee listed for this patent is TOYOTA JIDOSHA KABUSHIKI KAISHA. Invention is credited to Yuji Kariya, Misako Mochizuki.
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United States Patent |
10,876,745 |
Mochizuki , et al. |
December 29, 2020 |
Air conditioning register
Abstract
An air conditioning register includes a tube and a blade. An
inner side of the tube functions as a duct. The blade is located at
an outer side of the tube. The blade moves to change a distance
from the blade to a center axis of the tube. Movement of the blade
presses a portion of the tube between two ends in an axial
direction of the center axis from the outer side with the blade and
changes the duct in shape.
Inventors: |
Mochizuki; Misako (Miyoshi,
JP), Kariya; Yuji (Nisshin, JP) |
Applicant: |
Name |
City |
State |
Country |
Type |
TOYOTA JIDOSHA KABUSHIKI KAISHA |
Toyota |
N/A |
JP |
|
|
Assignee: |
TOYOTA JIDOSHA KABUSHIKI KAISHA
(Toyota, JP)
|
Family
ID: |
1000005268905 |
Appl.
No.: |
15/633,042 |
Filed: |
June 26, 2017 |
Prior Publication Data
|
|
|
|
Document
Identifier |
Publication Date |
|
US 20180128503 A1 |
May 10, 2018 |
|
Foreign Application Priority Data
|
|
|
|
|
Nov 7, 2016 [JP] |
|
|
2016-217250 |
|
Current U.S.
Class: |
1/1 |
Current CPC
Class: |
F24F
13/14 (20130101); F24F 1/0033 (20130101); F24F
1/0059 (20130101); F24F 13/082 (20130101); B60H
1/34 (20130101); F24F 13/06 (20130101); B60H
1/345 (20130101) |
Current International
Class: |
F24F
1/00 (20190101); B60H 1/34 (20060101); F24F
13/06 (20060101); F24F 13/14 (20060101); F24F
1/0059 (20190101); F24F 1/0033 (20190101); F24F
13/08 (20060101) |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
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|
|
|
|
3908612 |
|
Sep 1990 |
|
DE |
|
102007038212 |
|
Feb 2009 |
|
DE |
|
102008006158 |
|
Jul 2009 |
|
DE |
|
202010000678 |
|
May 2010 |
|
DE |
|
S59-157906 |
|
Oct 1984 |
|
JP |
|
H01-120043 |
|
Aug 1989 |
|
JP |
|
H05-083652 |
|
Nov 1993 |
|
JP |
|
2006-306365 |
|
Nov 2006 |
|
JP |
|
2008-080839 |
|
Apr 2008 |
|
JP |
|
2014-119246 |
|
Jun 2014 |
|
JP |
|
2016-78487 |
|
May 2016 |
|
JP |
|
Primary Examiner: Anderson, II; Steven S
Attorney, Agent or Firm: Oliff PLC
Claims
The invention claimed is:
1. An air conditioning register comprising: a tube, wherein an
inner side of the tube functions as a duct; a plurality of blades
located at an outer side of the tube and spaced equally around the
outer side of the tube in a circumferential direction of the tube,
each blade of the plurality of blades having an arcuate shape and
being located at a middle position in an axial direction of the
tube; and a transmission mechanism that comprises means for
pressing each of the plurality of blades to change a distance from
the blade to a center axis of the tube, wherein the transmission
mechanism is configured such that each blade of the plurality of
blades (i) can be spaced apart from the tube and (ii) moves when
pressed on to change the distance from the blade to the center axis
of the tube; and movement of each blade of the plurality of blades
presses, with the blade from the outer side, a portion of the tube
at the middle position and changes the duct in shape.
2. The air conditioning register according to claim 1, wherein the
tube is formed from an elastic material and includes a first end
and a second end, the air conditioning register further comprising:
a first case member to which the first end of the tube is fixed,
wherein the first case member limits deformation of the first end;
and a second case member to which the second end of the tube is
fixed, wherein the second case member limits deformation of the
second end.
3. The air conditioning register according to claim 2, wherein when
the plurality of blades moves toward the center axis of the tube, a
passage cross-sectional area of the duct decreases at the portion
of the tube that is pressed by the plurality of blades.
4. An air conditioning register comprising: a tube, wherein an
inner side of the tube functions as a duct and the tube includes a
first end and a second end; a blade located at an outer side of the
tube, the blade being configured to move to change a distance from
the blade to a center axis of the tube; a first case member to
which the first end of the tube is fixed, wherein the first case
member limits deformation of the first end; a second case member to
which the second end of the tube is fixed, wherein the second case
member limits deformation of the second end; and a biasing member
that applies tension to the tube and biases the first case member
and the second case member away from each other, wherein movement
of the blade presses, with the blade from the outer side, a portion
of the tube between the first and second ends in an axial direction
of the center axis and changes a shape of the duct.
5. An air conditioning register comprising: a tube, wherein an
inner side of the tube functions as a duct; a blade located at an
outer side of the tube, the blade being configured to move to
change a distance from the blade to a center axis of the tube; an
operation member located at the outer side of the tube in a radial
direction, wherein the operation member is rotatable in a
circumferential direction of the tube; a transmission mechanism
that moves the blade by transmitting power resulting from rotation
of the operation member to the blade; and a restriction member
located at two sides of the blade in the circumferential direction,
wherein the restriction member restricts movement of the blade in
the circumferential direction, wherein movement of the blade
presses, with the blade from the outer side, a portion of the tube
between two ends of the tube in an axial direction of the center
axis and changes a shape of the duct, the blade includes a guide
hole, the guide hole is inclined relative to the circumferential
direction to gradually extend toward an inner side in the radial
direction from one of two ends of the guide hole in the
circumferential direction to the other end, and the transmission
mechanism includes a shaft coupled to the operation member and
inserted through the guide hole.
6. The air conditioning register according to claim 5, further
comprising a holding portion, wherein one of two longitudinal ends
of the guide hole, located at the inner side in the radial
direction, is a first end, the other one of the longitudinal ends,
located at the outer side in the radial direction, is a second end,
and the holding portion keeps the shaft located closer to the
second end than the first end in the guide hole.
7. The air conditioning register according to claim 6, wherein the
holding portion is a projection that projects toward the outer side
in the radial direction from a radially inner circumferential wall
of the guide hole, the projection includes a surface facing the
first end and inclined toward the second end in the circumferential
direction to be closer to the second end at positions located
toward the outer side in the radial direction, the projection
includes a surface facing the second end and inclined toward the
first end in the circumferential direction to be closer to the
first end at positions located toward the outer side in the radial
direction, and the projection engages the shaft on the surface
facing the second end and keeps the shaft located closer to the
second end than the first end.
Description
BACKGROUND OF THE INVENTION
The present invention relates to an air conditioning register.
Japanese Laid-Open Patent Publication No. 2014-119246 discloses an
example of an air conditioning register installed in a vehicle. The
air conditioning register includes a tube. The inner side of the
tube functions as a duct. Air flows through the duct before being
blown into the passenger compartment.
As shown in FIGS. 9 and 10, the register described in the document
changes the mode in which air is blown out of an outlet 53 by
changing the directions of movable fins 51 and 52 that are arranged
in a duct 50. For example, when the movable fins 51 and 52 are
arranged in a direction in which air flows through the duct 50 as
shown by the solid line in FIG. 9, the spreading of the air blown
out of the outlet 53 is limited. When the movable fins 51 and 52
are arranged orthogonal to the direction in which air flows in the
duct 50 as shown in FIG. 10, the duct 50 is partially closed by the
movable fins 51 and 52. This narrows the duct 50. Thus, the air
flowing through the narrowed portion in the duct 50 spreads toward
the outlet 53. This easily spreads the air blown out of the outlet
53. In this manner, the directions of the movable fins 51 and 52
are changed in the duct 50 to shift between a spot airflow mode
that limits the spreading of the air blown into the passenger
compartment and a diffusion airflow mode that facilitates the
spreading of the air blown into the passenger compartment.
In the above air conditioning register, when air is blown out of
the outlet 53 in the spot airflow mode, the movable fins 51 and 52
in the duct 50 interfere with the flow of air.
Fins interfere with the flow of air when the direction of air does
not need to be changed not only in a structure in which the fins
are used to switch between the spot airflow mode and the diffusion
airflow mode but also in a structure in which the fins are arranged
in a duct to adjust the direction of the air blown out of the
outlet.
SUMMARY OF THE INVENTION
It is an object of the present invention to provide an air
conditioning register that changes a mode of blowing air out of a
tube into a passenger compartment and supplies air efficiently.
To solve the above problem, an air conditioning register according
to a first aspect of the present invention includes a tube and a
blade. An inner side of the tube functions as a duct. The blade is
located at an outer side of the tube. The blade moves to change a
distance from the blade to a center axis of the tube. Movement of
the blade presses a portion of the tube between two ends in an
axial direction of the center axis from the outer side with the
blade and changes the duct in shape.
Other aspects and advantages of the present invention will become
apparent from the following description, taken in conjunction with
the accompanying drawings, illustrating by way of example the
principles of the invention.
BRIEF DESCRIPTION OF THE DRAWINGS
The invention, together with objects and advantages thereof, may
best be understood by reference to the following description of the
presently preferred embodiments together with the accompanying
drawings in which:
FIG. 1 is a cross-sectional view schematically showing an air
conditioning register according to one embodiment of the present
invention;
FIG. 2 is a perspective view showing the air conditioning
register;
FIG. 3 is an enlarged plan view showing a guide hole in a blade of
the air conditioning register;
FIG. 4 is a cross-sectional view schematically showing a state in
which the air conditioning register is in a spot airflow mode;
FIG. 5 is a cross-sectional view schematically showing a state in
which the air conditioning register is in a diffusion airflow
mode;
FIG. 6 is a schematic view showing a transmission mechanism and a
tube in another embodiment of the air conditioning register;
FIG. 7 is a cross-sectional view schematically showing a further
embodiment of the air conditioning register;
FIG. 8 is a schematic view showing a blade in still another
embodiment of an air conditioning register and a blade movement
mode;
FIG. 9 is a cross-sectional view schematically showing a state in
which a conventional air conditioning register is in a spot airflow
mode; and
FIG. 10 is a cross-sectional view schematically showing a state in
which the conventional air conditioning register is in a diffusion
airflow mode.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
One embodiment of an air conditioning register of the present
invention applied to an in-vehicle air conditioning register will
now be described with reference to FIGS. 1 to 5.
FIGS. 1 and 2 show an air conditioning register 10 that guides air
flowing from an in-vehicle air conditioning device into a passenger
compartment 100. As shown in FIGS. 1 and 2, the air conditioning
register 10 includes a cylindrical tube 11. The inner side of the
tube 11 functions as a duct 12 through which air flows from the air
conditioning device. The tube 11 includes an inner circumferential
surface 11A defining the duct 12. The tube 11 is formed from an
elastic material such as elastomer.
Further, the air conditioning register 10 includes a ring-shaped
first case member 13 and a ring-shaped second case member 14. The
first case member 13 is fixed to an end 111 of the tube 11 serving
as a first end that faces the passenger compartment 100. The second
case member 14 is fixed to an end 112 of the tube 11 serving as a
second end located at a side opposite to the passenger compartment
100. The first case member 13 is formed from a material that is
less deformable than the tube 11. The entire circumference of the
end 111 of the tube 11 is joined with the inner side of the first
case member 13. Thus, the first case member 13 limits deformation
of the end 111 of the tube 11. In the same manner, the second case
member 14 is formed from a material that is less deformable than
the tube 11. The entire circumference of the end 112 of the tube 11
is joined with the inner side of the second case member 14. Thus,
the second case member 14 limits deformation of the end 112 of the
tube 11.
The first case member 13 is supported by a panel member 101 that
defines the passenger compartment 100. Air flows through the duct
12 of the tube 11 before being blown from the inner side of the
first case member 13 into the passenger compartment 100.
An operation ring 15 serving as an operation member is arranged at
an outer side of the first case member 13 in a radial direction.
The operation ring 15 is located in the passenger compartment 100
so that an occupant can operate the operation ring 15. The
operation ring 15 is rotated along an outer circumferential surface
of the first case member 13 in a circumferential direction of the
tube 11 as shown by the arrows in FIG. 2.
Three blades 16 are arranged at the outer side of the tube 11 in
the radial direction. The three blades 16 are located at a middle
position between the two case members 13 and 14 in an axial
direction of the tube 11. The three blades 16 are spaced apart from
one another in the circumferential direction around the tube 11.
The portion of the tube 11 located at the same position in the
axial direction as the blades 16 is referred to as the
predetermined portion 113.
As shown in FIGS. 2 and 3, each blade 16 is an arcuate plate. Each
blade 16 is arranged so that a thickness-wise direction of each
blade 16 corresponds to the axial direction of the tube 11. A guide
hole 17 extends through a circumferentially middle portion of each
blade 16. Referring to FIG. 3, one of the two ends of the guide
hole 17 is referred to as the first end 171 (right end), and the
other end (left end) is referred to as the second end 172. In this
case, the first end 171 is located at the inner side of the second
end 172 in the radial direction. The guide hole 17 is inclined
relative to the circumferential direction and extended toward the
inner side in the radial direction from the second end 172 toward
the first end 171.
As shown in FIG. 2, a restriction member 18 is arranged between the
blades 16 that are adjacent to each other in the circumferential
direction. The three restriction members 18 are supported by the
two case members 13 and 14 to restrict movement of the blades 16 in
the circumferential direction and the radial direction. The
restriction members 18 restrict movement of the blades 16 in the
circumferential direction.
As shown in FIGS. 1 and 2, the air conditioning register 10
includes a transmission mechanism 20 that moves each blade 16 in
the radial direction by transmitting, to each blade 16, power
generated when an occupant rotates the operation ring 15. The
transmission mechanism 20 includes shafts 22 supported by the
operation ring 15. The number of the shafts 22 is the same as that
of the blades 16.
Each shaft 22 extends in the axial direction of the tube 11 through
the guide hole 17 of the corresponding blade 16. As shown in FIG.
1, the distal end (left end) of each shaft 22 is fixed to a first
support 23. Further, a second support 24 is fixed at a position of
each shaft 22 that is slightly separated from the corresponding
blade 16 toward the basal end (right end). That is, each blade 16
is located between the first support 23 and the second support 24
of the corresponding shaft 22. Thus, the first support 23 and the
second support 24 restrict movement of the blade 16 in the axial
direction of the shaft 22.
When the operation ring 15 is rotated in the circumferential
direction, each shaft 22 moves in synchronization with the
operation ring 15. Movement of each blade 16 in the circumferential
direction is restricted by the restriction member 18. Thus, the
blades 16 move in the radial direction. When the shaft 22 is
located at the first end 171 of the guide hole 17 as shown by the
solid line in FIG. 3, the blade 16 does not abut against an outer
circumferential surface 11B of the tube 11 as shown in FIG. 4. When
the operation ring 15 is rotated in the circumferential direction
from the state shown in FIG. 3, the shaft 22 moves in the
circumferential direction toward the second end 172 in the guide
hole 17 as shown by the solid-line arrows. The blade 16 is pressed
by the shaft 22 toward the inner side in the radial direction and
moved toward the center axis Z of the tube 11. Then, the blade 16
abuts against the outer circumferential surface 11B of the tube 11
and presses the outer circumferential surface 11B. This elastically
deforms and moves the predetermined portion 113 of the tube 11,
which is pressed by the blade 16, toward the inner side in the
radial direction as shown in FIG. 5. The blades 16 are arranged
around the tube 11 in the circumferential direction. Thus, the
diameter at the predetermined portion 113 is decreased. That is,
the circumferential position of the circumferential surface of the
predetermined portion 113 moves toward the center axis Z of the
tube 11.
In a state in which the blade 16 presses the predetermined portion
113 of the tube 11, when the blade 16 further moves toward the
inner side in the radial direction, the diameter at the
predetermined portion 113 further decreases. When the shaft 22
reaches the second end 172 in the guide hole 17, the blade 16 does
not further move toward the inner side in the radial direction.
Thus, the diameter at the predetermined portion 113 is the smallest
in this state, and the passage cross-sectional area of the
predetermined portion 113 is the smallest.
When the operation ring 15 is rotated in the opposite
circumferential direction from a state in which the shaft 22 is
located at the second end 172, the shaft 22 moves in the
circumferential direction toward the first end 171 in the guide
hole 17 as shown by the broken-line arrows in FIG. 3. The
resiliency of the tube 11 moves the blade 16 toward the outer side
in the radial direction. Thus, the predetermined portion 113 of the
tube 11 moves toward the outer side in the radial direction. This
gradually increases the diameter at the predetermined portion 113.
When the shaft 22 reaches the first end 171 in the guide hole 17,
the blade 16 does not abut against the tube 11 as shown in FIG. 4.
Thus, a pressing force is not applied from the blade 16 to the tube
11. In this case, the diameter at the predetermined portion 113 is
substantially equal to that at the end 111 of the tube 11.
As shown in FIG. 3, the air conditioning register 10 includes a
holding portion 30 that keeps the shaft 22 located closer to the
second end 172 than the first end 171. The holding portion 30 is a
projection 31 that projects toward the outer side in the radial
direction from a radially inner circumferential wall 17A1 of the
guide hole 17. The surface (right surface) of the projection 31 is
a first inclined surface 32 facing the first end 171 and inclined
toward the second end 172 in the circumferential direction to be
closer to the second end 172 at positions located toward the outer
side in the radial direction. The surface (left surface) of the
projection 31 is a second inclined surface 33 facing the second end
172 and inclined toward the first end 171 in the circumferential
direction to be closer to the first end 171 at positions located
toward the outer side in the radial direction.
The straight line L1 shown by the broken line in FIG. 3 extends in
a longitudinal direction of the guide hole 17. The inclination
angle .theta.2 of the second inclined surface 33 relative to the
longitudinal direction of the guide hole 17 and the inclination
angle .theta.1 of the first inclined surface 32 relative to the
longitudinal direction of the guide hole 17 are less than
90.degree.. The inclination angle .theta.2 of the second inclined
surface 33 is greater than the inclination angle .theta.1 of the
first inclined surface 32. Thus, it is more difficult for the shaft
22 to move beyond the projection 31 when the shaft 22 moves from
the second end 172 to the first end 171 than when the shaft 22
moves from the first end 171 to the second end 172.
The operation and advantage of the air conditioning register 10 of
the present embodiment will now be described.
When each shaft 22 is located at the first end 171 of the
corresponding guide hole 17, the three blades 16 do not abut
against the tube 11 as shown in FIG. 4. Thus, a pressing force is
not applied from each blade 16 to the tube 11. Accordingly, the
diameter at the predetermined portion 113 of the tube 11 is
substantially the same as the inner diameter at the end 111 of the
tube 11. In this case, the diameter of the duct 12 at the inner
side of the tube 11, that is, the radial position of the
circumferential surface of the duct, does not change over the
entire length of the duct 12. Further, in this case, air flows
through the duct 12 along the inner circumferential surface 11A of
the tube 11 toward the end of the duct 12 located proximate to the
passenger compartment 100. As shown by the arrows in FIG. 4, this
limits the spreading of the air blown out of the tube 11 toward the
passenger compartment 100. The airflow mode that limits the
spreading of air blown out of the tube 11 is referred to as the
"spot airflow mode."
When the operation ring 15 is rotated by an occupant in a state in
which air is blown out of the tube 11 into the passenger
compartment 100 in the spot airflow mode, the shafts 22 are moved
in the circumferential direction. Thus, when each shaft 22 presses
the radially inner circumferential wall 17A1 of the corresponding
guide hole 17, each blade 16 moves toward the inner side in the
radial direction. As a result, as shown in FIG. 5, each blade 16
abuts against the predetermined portion 113 of the tube 11. Thus,
each blade 16 presses the predetermined portion 113 of the tube 11.
This decreases the diameter at the predetermined portion 113.
Even when the inner diameter at the predetermined portion 113 of
the tube 11 decreases, the diameter at the end 111 of the tube 11
fixed to the first case member 13 does not decrease. Thus, when
each blade 16 presses the predetermined portion 113, as shown in
FIG. 5, the diameter of the duct 12 at the inner side of the tube
11, that is, the radial position of the circumferential surface of
the duct, is the smallest at the portion corresponding to the
predetermined portion 113 and gradually increases from the
predetermined portion 113 of the tube 11 toward the end located
proximate to the passenger compartment 100. As a result, as shown
by the arrows in FIG. 5, the air that passes through the portion
where the diameter of the duct 12 is the smallest spreads toward
the outer side in the radial direction along the inner
circumferential surface 11A of the tube 11 as the end of the duct
12 proximate to the passenger compartment 100 becomes closer. Thus,
the air flowing through the duct 12 and blown out of the tube 11
into the passenger compartment 100 spreads easily. The airflow mode
that facilitates the spreading of the air blown out of the tube 11
is referred to as the "diffusion airflow mode."
When switching the diffusion airflow mode to the spot airflow mode,
the operation ring 15 is operated and rotated in the
circumferential direction by an occupant so that the shaft 22 moves
toward the first end 171 in the guide hole 17. When the operation
ring 15 is rotated in this manner, the resiliency of the tube 11
moves each blade 16 toward the outer side in the radial direction.
This increases the diameter at the predetermined portion 113 of the
tube 11. When the shaft 22 reaches the first end 171 in the guide
hole 17, each blade 16 does not abut against the tube 11 as shown
in FIG. 4. This limits the spreading of the air blown out of the
tube 11 into the passenger compartment 100.
In this manner, movement of each blade 16 located outside the duct
12 in the radial direction allows for the shifting between the spot
airflow mode and the diffusion airflow mode. Thus, the vehicle
occupant can change the air blow mode by operating the operation
ring 15 without a member arranged in the duct to change the mode
for blowing air into the passenger compartment 100.
Further, since there is no member in the duct 12 used to change the
air blow mode, the efficiency for supplying air when air is blown
in the spot airflow mode particularly increases as compared to an
air conditioning register that includes a member in the duct to
change the air blow mode. This increases the amount of air blown
into the passenger compartment 100 with less power consumption and
improves the efficiency for using energy in a vehicle.
Further, each restriction member 18 is arranged between the blades
16 that are adjacent to each other in the circumferential
direction. Thus, when the rotation of the operation ring 15 moves
each shaft 22 in the circumferential direction, movement of the
blades 16 with the shafts 22 is restricted. As a result, the
movement of each shaft 22 when the vehicle occupant rotates the
operation ring 15 efficiently moves each blade 16 in the radial
direction.
In addition, the radially inner circumferential wall 17A1 of the
guide hole 17 includes the projection 31 that keeps the shaft 22
located closer to the second end 172 than the first end 171 in the
guide hole 17. Thus, the shaft 22 engages the second inclined
surface 33 of the projection 31 after the vehicle occupant stops
operating the operation ring 15 after moving the shaft 22 to the
second end 172 by operating the operation ring 15. More
specifically, when the operation ring 15 is rotated to move the
blade 16 toward the inner side in the radial direction, the shaft
22 abuts against the first inclined surface 32 of the projection
31. The first inclined surface 32 is inclined to be closer to the
second end 172 at positions located toward the outer side in the
radial direction. Thus, when the operation ring 15 is further
operated, the shaft 22 moves beyond the projection 31. This
arranges the shaft 22 between the projection 31 and the second end
172 in the guide hole 17. When the shaft 22 is located between the
projection 31 and the second end 172 in this manner, the shaft 22
engages the second inclined surface 33 of the projection 31. Thus,
even when each blade 16 receives the resilient force of the tube
11, the shaft 22 remains closer to the second end 172 than the
first end 171. This restricts movement of the blade 16 toward the
outer side in the radial direction while countering the resiliency
of the tube 11. As a result, air is continuously blown in the
diffusion airflow mode.
Further, the second inclined surface 33 of the projection 31 is
inclined to be closer to the first end 171 at positions located
toward the outer side in the radial direction. Thus, when the
operation ring 15 is rotated, the shaft 22 moves from between the
projection 31 and the second end 172 toward the first end 171 in
the guide hole 17. In this manner, rotation of the operation ring
15 moves the blade 16 toward the outer side in the radial
direction. This moves the shaft 22 beyond the projection 31 to the
first end 171 and disengages the second inclined surface 33 of the
projection 31 from the shaft 22. The inclination angle .theta.1 of
the first inclined surface 32 of the projection 31 and the
inclination angle .theta.2 of the second inclined surface 33 of the
projection 31 are less than 90.degree.. Thus, even when an occupant
operates the operation ring 15 to move the shaft 22 from the first
end 171 to the second end 172 in the guide hole 17 or from the
second end 172 to the first end 171 in the guide hole 17, rotation
of the operation ring 15 in the circumferential direction moves the
shaft 22 beyond the projection 31.
It should be apparent to those skilled in the art that the present
invention may be embodied in many other specific forms without
departing from the spirit or scope of the invention. Particularly,
it should be understood that the present invention may be embodied
in the following forms.
As long as movement of the shafts 22 in the circumferential
direction moves the blades 16 in the radial direction and deforms
the tube 11, the blades 16 may be allowed to be moved by a certain
amount in the circumferential direction.
The inclination angle .theta.2 of the second inclined surface 33 of
the projection 31 may be less than or equal to the inclination
angle .theta.1 of the first inclined surface 32 of the projection
31 as long as engagement with the shaft 22 keeps the shaft 22
located closer to the second end 172 than the first end 171 in the
guide hole 17.
The holding portion 30 may have any shape other than the shape of
the projection 31 as long as the holding portion 30 keeps the shaft
22 located closer to the second end 172 than the first end 171 in
the guide hole 17. For example, the holding portion 30 may be a
recess located in the radially inner circumferential wall 17A1 of
the guide hole 17. In this case, when the shaft 22 that is moving
in the circumferential direction is received in the recess, the
shaft 22 engages a circumferential surface of the recess. This
keeps the shaft 22 closer to the second end 172 than the first end
171 in the guide hole 17. This structure also separates the shaft
22 from the recess and moves the blade 16 in the radial direction
when the operation ring 15 is rotated by a vehicle occupant.
In the above embodiment, the radially inner circumferential wall
17A1 of the guide hole 17 includes only one projection 31, which
keeps the shaft 22 located closer to the second end 172 than the
first end 171. However, a further projection that is separate from
the projection 31 may be arranged between the projection 31 of the
radially inner circumferential wall 17A1 and the first end 171. In
this case, the further projection keeps the shaft 22 located
between the first end 171 of the guide hole 17 and the projection
31. This structure allows for adjustment of the degree of air
spreading in the passenger compartment 100. The number of
projections may be three or more.
As long as a transmission mechanism of an air conditioning register
moves each blade 16 in the radial direction by transmitting power
resulting from movement of an operation member to the blade 16, the
transmission mechanism 20 does not have to be structured as
described in the above embodiment. FIG. 6 shows an example of an
air conditioning register including another transmission mechanism.
As shown in FIG. 6, an air conditioning register 210 includes an
operation member 215 that moves in an axial direction (vertical
direction) of the tube 11. The air conditioning register 210
includes a transmission mechanism 220 that transmits the power
resulting from axial movement of the operation member 215 to blades
216. The transmission mechanism 220 includes a transmission member
221 extending in the axial direction and including an upper end
that is fixed to the operation member 215. The transmission member
221 includes a lower end having a claw 222 that projects toward the
inner side (left side) in the radial direction. The claw 222
includes a distal end surface (left end surface) serving as an
action surface 223 inclined toward the outer side (right side) in
the radial direction at positions located farther from the
operation member 215. Further, a surface of each blade 216 located
at the outer side in the radial direction is an inclined surface
217 that is inclined toward the outer side in the radial direction
at positions located farther from the operation member 215.
When the operation member 215 moves in the axial direction, the
action surface 223 of the claw 222 is abutted against and pressed
by the inclined surface 217 of each blade 216 as shown by the
broken line in FIG. 6, the claw 222 presses the blade 216 toward
the inner side in the radial direction. As a result, the blade 216
moves toward the inner side in the radial direction and presses the
predetermined portion 113 of the tube 11. This deforms the tube 11
so that the diameter of the predetermined portion 113 decreases.
This structure also changes the mode for blowing air out of the
tube 11 and into the passenger compartment 100 by moving each blade
216 located outside the duct 12.
As long as blades are moved in the radial direction, an air
conditioning register may include an electric actuator that moves
the blades. In this case, the actuator is operated to change the
radial position of each blade. This changes the shape of the duct
12 located inside the tube 11 and changes the mode for blowing air
out of the tube 11 and into the passenger compartment 100.
Further, when the electric actuator is used to move the blades,
each blade may be moved by a single actuator. Alternatively, a
plurality of actuators that respectively correspond to the blades
may be arranged. When using a plurality of actuators, the radial
positions of the blades are separately controlled. This allows air
to be blown out of the tube 11 and into the passenger compartment
100 in a number of modes.
As long as a tube is pressed and deformed by blades, the tube does
not have to be formed from elastomer and may be formed from another
flexible material. FIG. 7 shows an example of an air conditioning
register 310 including a tube 311. In this example, blades 316 are
moved by an actuator 320. The air conditioning register 310 shown
in FIG. 7 includes a plurality of biasing members 321 located
between the blades 316 that are adjacent to each other. Each
biasing member 321 biases the first case member 13 and the second
case member 14 away from each other and applies tension to the tube
311.
In this structure, when each blade 316 moves toward the inner side
of the tube 311 in the radial direction, a portion of the tube 311
pressed by the blade 316 is moved toward the inner side in the
radial direction against the tension of the tube 311. The second
case member 14 moves against a biasing force of each biasing member
321 and shortens the distance between the second case member 14 and
the first case member 13. Even when the blade 316 moves, the first
case member 13 and the second case member 14 limit deformation of
two ends of the tube 311. That is, this structure deforms the
portion of the tube 311 pressed by the blade 316 against the
tension of the tube 311 and changes the shape of a duct 312 without
greatly deforming the two ends of the tube 311. Thus, the mode for
blowing air blown into the passenger compartment 100 can be changed
using the inclination of an inner circumferential surface of the
tube 311 from the portion of the tube 311 that is pressed and
deformed by the blade 316 to the end located proximate to the
passenger compartment 100. When the blade 316 moves toward the
outer side in the radial direction, the portion of the tube 311
pressed by the blade 316 is moved toward the outer side in the
radial direction by the tension of the tube 311. The biasing force
of the biasing member 321 moves the second case member 14 to
increase the distance between the second case member 14 and the
first case member 13.
As long as a tube is deformed by movement of blades, the blades may
be moved in a direction that differs from the radial direction. For
example, as shown in FIG. 8, disk-shaped blades 416 extending in an
axial direction of a tube 411 may be supported by shafts 417 to be
rotatable in the direction shown by the arrows. In this case, each
blade 416 is supported by the corresponding shaft 417 at a position
that differs from the center 416A. In addition, when X1 represents
the length of a straight line extending from the center of the
shaft 417 through the center 416A to an outer circumferential
surface of the blade 416 and X2 represents the shortest distance
from the center of the shaft 417 to an outer circumferential
surface of the tube 411, the first length X1 is greater than the
second length X2. In this structure, rotation of the shaft 417
rotates the blade 416 about the shaft 417 as shown by the broken
line in FIG. 8. In this manner, when rotation of the blade 416
changes the distance from the center axis of the tube 411 to the
blade 416, the tube 411 is deformed, and a duct located inside the
tube 411 is changed in shape.
As long as the shapes of a tube and a duct located inside the tube
are changed by movement of blades, any number of blades may be
arranged. Further, when the tube is pressed by a plurality of
blades, the blades may be located at different positions in an
axial direction of the tube.
As long as the inner side of a tube functions as a duct, the tube
does not have to be cylindrical and may be box-shaped.
The present examples and embodiments are to be considered as
illustrative and not restrictive, and the invention is not to be
limited to the details given herein, but may be modified within the
scope and equivalence of the appended claims.
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